AU2004267143A1 - Flow channel for liquids - Google Patents

Flow channel for liquids Download PDF

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Publication number
AU2004267143A1
AU2004267143A1 AU2004267143A AU2004267143A AU2004267143A1 AU 2004267143 A1 AU2004267143 A1 AU 2004267143A1 AU 2004267143 A AU2004267143 A AU 2004267143A AU 2004267143 A AU2004267143 A AU 2004267143A AU 2004267143 A1 AU2004267143 A1 AU 2004267143A1
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AU
Australia
Prior art keywords
flow
flow channel
cross
section
region
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU2004267143A
Inventor
Aloys Wobben
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Individual
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Individual
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Filing date
Publication date
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Publication of AU2004267143A1 publication Critical patent/AU2004267143A1/en
Abandoned legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15DFLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00Influencing flow of fluids
    • F15D1/02Influencing flow of fluids in pipes or conduits
    • F15D1/06Influencing flow of fluids in pipes or conduits by influencing the boundary layer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15DFLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00Influencing flow of fluids
    • F15D1/02Influencing flow of fluids in pipes or conduits
    • F15D1/06Influencing flow of fluids in pipes or conduits by influencing the boundary layer
    • F15D1/065Whereby an element is dispersed in a pipe over the whole length or whereby several elements are regularly distributed in a pipe
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15DFLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00Influencing flow of fluids
    • F15D1/02Influencing flow of fluids in pipes or conduits
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/0753Control by change of position or inertia of system
    • Y10T137/0777With second control

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Water Treatment By Electricity Or Magnetism (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

Australia VERIFICATION OF TRANSLATION I, Michael Wallace Richard Turner, Bachelor of Arts, Chartered Patent Attorney, European Patent Attorney, of 1 Horsefair Mews, Romsey, Hampshire SO51 8JG, England, do hereby declare that I am the translator of the attached Amended page in the German language of International Application PCT/EP2004/002961 and I state that the following is a true translation to the best of my knowledge and belief. MWR Turner Signed this 3 9kcay of- *e 2005 Bremen 18th May 2005 Our ref: WA 2468-03WO MAG/mwu Direct dial: 0421/36 35 12 Applicant/proprietor: WOBBEN, Aloys Office ref: PCT/EP2004/002 9 6 1 New claim 1 1. A flow channel for liquids characterised in that at least one wall defining the flow channel is of such a configuration that when a liquid flows therethrough at least one flow region is produced which has an axial and simultaneous tangential flow component, wherein the flow cross-section of the flow channel is non-cylindrical and is twisted in itself in the axial direction so that when the liquid flows therethrough a spiral-form flow is produced at least in region-wise manner.
Australia VERIFICATION OF TRANSLATION I, Michael Wallace Richard Turner, Bachelor of Arts, Chartered Patent Attorney, European Patent Attorney, of 1 Horsefair Mews, Romsey, Hampshire SO51 8JG, England, do hereby declare that I am the translator of the attached specification in the German language of International Application PCT/EP2004/002961 and I state that the following is a true translation to the best of my knowledge and belief. M W R Turner Signed this,0o-day of 2005 Aloys WOBBEN Argestrasse 19, 26607 Aurich Flow channel for liquids 5 The invention concerns a flow channel for liquids. As is known liquids or also gases are passed through flow channels of the most widely varying configurations in the most widely different areas of life. The purpose in that respect is frequently to transport substances 10 and/or energy. Examples of flow channels for liquids are pipes for example in domestic technology or process or energy technology or flow channels in fluid flow machines such as for example water turbines or sewage treatment plants. In the biological field flow channels are embodied for example in the form of veins for transporting blood. 15 As state of the art attention is directed at this juncture generally to the following publications: DE 198 06 513; WO 01/18406 Al; WO 00/38591 A2; US No 2 935 906 and US No 1 958 577. A decisive characteristic parameter of flows through flow channels is the flow resistance which is governed substantially by friction and changes 20 in direction and which is frequently expressed in the form of standardised characteristic values such as the drag resistance coefficient. Taking account of the flow resistance is of central importance in terms of designing flow channels such as pipelines and the dimensioning of pumps or other pressure-generating units. 25 It will be appreciated that the flow resistance and the frictional losses which occur in respect of the flow must be minimised as much as possible so that for example the amount of energy required for pumping and thus ultimately the energy consumption for an installation can be kept as low as possible. That is to be taken into consideration in the design of flow 30 channels. The object of the present invention is to provide a flow channel for liquids or also gases, which is of such a design that the lowest possible losses occur in the flow, in particular low frictional losses. A further aim of ,1 2 the invention is to provide a flow channel for liquids, in which different flow regions are set. The invention attains that object in a flow channel of the kind set forth in the opening part of this specification in that at least one wall 5 defining the flow channel is of such a configuration that when a liquid flows therethrough at least one flow region is produced which has an axial and simultaneous tangential flow component. Surprisingly it was found in tests that, by means of a flow channel according to the invention, on the basis of the wall configuration thereof, a 10 flow with an axial and tangential flow component is produced at least in portion-wise manner, whereby the flow resistance is significantly reduced in comparison with conventional flow channels. That reduction in the flow resistance advantageously provides that the energy losses in the flow, the pressure losses and the resistance coefficient are reduced. Therefore a 15 lower pump output is required to produce a given volume flow or mass flow of a liquid, than in the case of conventional flow channels. In that way for example in the case of pipelines the pump output to be applied can be markedly reduced. In the case also of fluid flow machines, hydraulic power stations or the like however the flow losses can also be reduced in 20 accordance with the invention and thus the levels of efficiency can be increased. Preferably a circulating spiral flow is produced in region-wise manner or completely. Experimental investigations have shown that lower flow resistances and thus flow losses occur by virtue of a wall configuration 25 which causes a kind of circulating spiral flow through the flow channel. In accordance with a particularly preferred embodiment it is proposed that the length of a tube portion which is completely wound once in itself (wavelength) is in a given ratio to the length of the smallest bisector of the cross-sectional area of the flow channel, which is in the 30 region of 6 to 7, particularly preferably in the region of 6.44. Due to the non-cylindrical configuration of the flow cross-section and twisting or winding in the axial direction, it is possible to produce an at least partially 3 spiral-like flow with axial and tangential flow components with a low level of flow resistance in a structurally simple manner. It has been found on the basis of tests that, with the above-specified ratio between wavelength and extent of the cross-sectional area, 5 particularly low resistance coefficients can be achieved. An embodiment which is particularly preferred from the structural point of view and in terms of flow technology is distinguished in that the wall delimiting the flow channel is so shaped that the free flow cross-section of the flow tube is substantially oval. Such an oval configuration with at the same time 10 twisting in itself of the flow cross-section can be particularly well implemented in a flow tube. In a development it is proposed that the ratio of the length of the longer axis of the oval flow cross-section to the length of the shorter axis of the flow cross-section is markedly greater than 1, preferably greater than 15 or about q2. In that way too the resistance coefficients of the flow channel can be minimised. In a further preferred embodiment it is proposed that the flow cross section decreases or enlarges in the flow direction. In that way, while retaining the advantages according to the invention, it is possible to 20 increase or reduce respectively the flow conditions and in particular the flow speed. The invention further attains its object or is further developed by a flow channel for liquids, which is so designed that within the channel when a liquid flows therethrough substantially two flow regions are produced, 25 which do not or which scarcely interpenetrate and which are wrapped around in the nature of a double helix. By virtue of such a configuration of the flow channel and a flow with substantially two flow regions, it is also possible to achieve low levels of flow resistance so that ultimately pump outputs are reduced and the levels 30 of efficiency of fluid flow machines are improved. In addition different phases of a flow, for example different liquids, can be passed in partially separated relationship through a flow channel or divide into at least partially different phases even when flowing through the flow channel. Such 4 a separation can occur for example by different constituents of a liquid with different material properties such as densities or viscosities preferably moving in given regions of the flow cross-section so that separation of a mixture into its constituent parts can occur. 5 A further development of the flow channel according to the invention provides that within each flow region there are produced further sub-flow regions which in turn are again intertwined with each other. In that way the flow conditions can be further improved and possibly the above-described separation effects can be enhanced. 10 In accordance with a further advantageous configuration it is proposed that the two core flow channels are of a substantially round configuration and form a main fluid flow and that produced in the region of the flow tube which is not occupied by the main flow cores are one or more secondary flows, wherein no or preferably only a slight fluid exchange takes 15 place between a main flow and a secondary flow area and foreign bodies in the entire fluid flow are preferably transported in the secondary flow area. In that way also solid and liquid or different liquid phases of the flow can be formed. The invention is described hereinafter by means of embodiments by 20 way of example with reference to the accompanying drawings in which: Figure 1 is a diagrammatic view of a flow channel provided in a flow tube, Figures 2a - f show different examples of flow channels according to the invention, 25 Figure 3 shows measurement results of tests with flow channels according to the invention, Figure 4 shows a flow with different flow regions, which is diagrammatically illustrated in a flow channel according to the invention, and 30 Figure 5 is a diagrammatic cross-sectional view of the flow shown in Figure 4. Figure 1 is a side view of an embodiment of a flow tube 2 in which a flow channel 4 according to the invention is provided. Fluids, that is to say 5 liquids or gases, can flow through the tube 2 or the flow channel 4. This can also involve multi-phase flows with different liquid components and with solid bodies such as particles or the like. In addition for example a three phase flow with liquid, gaseous and solid components can also flow through 5 the flow channel 4. The tube 2 can be made of plastic material or metal. The tube 2 is preferably of such a configuration that the flow cross section is substantially oval, as is shown in the diagrammatic views of Figure 2a) and 2b). As Figure 1 diagrammatically shows, the tube 2 is wound or twisted in itself in the axial direction, that is to say in the 10 direction of the longitudinal axis 3. In the portion of the tube 2 shown in Figure 1, the extent of the twist is illustrated by the line 5 which, over the illustrated length of the tube portion, performs a complete revolution through 360 degrees; that length of a single complete twist is also referred to herein as the wavelength. In 15 the side view of Figure 1, tube portions of greater width and smaller width are afforded by virtue of the oval cross-section (Figures 2a and 2b) and the twist. The lengths of the shorter and longer axes of the substantially oval flow cross-section are entered in Figures 2a and 2b. By means of experimental investigations it was found out that the ratio of the length of 20 the longer axis a to the shorter axis b should preferably be greater than or equal to /2. The configuration of the wall of the tube 2 shown in Figure 2a is curved somewhat less in comparison with the configuration of the walls of the embodiment shown in Figure 2b. When a liquid flows through the flow channel 4 according to the 25 invention, a flow is produced in the flow channel 4, which not only has a flow component in the axial direction, that is to say in the direction of the axis 3, but also a flow component in a tangential direction with respect to the axis 3. That arises out of the twisted configuration of the flow channel 4 or the tube 2. That is diagrammatically illustrated in Figures 1 and 2a by 30 arrows 7. Accordingly that produces in the flow channel 4 substantially a circulating, spiral-shaped flow through the tube 2. The alternative flow cross-sections shown in Figures 2c - f equally result in a flow according to the invention with an axial flow component and 6 a tangential flow component and accordingly a kind of spiral flow in the flow channel 4. Figure 2c shows a rectangular flow cross-section, Figure 2d shows a square flow cross-section, Figure 2e shows a triangular flow cross section and Figure 2f shows an octagonal flow cross-section. A hexagonal 5 configuration for the flow cross-section or a corresponding flow tube 2 is also possible in accordance with the invention. These embodiments by way of example are also preferably of such a configuration that the flow cross section is twisted in itself in the axial direction (axis 3). The ratio of the wavelength to the length of the smallest bisector of 10 the cross-sectional area of the flow cross-section 4 is in a given ratio which is in the region of 6 to 7. Results of experimental investigations with flow channels according to the invention are illustrated in Figure 3. Measurements of the output of a pump with conventional cylindrical tubes and with oval tubes twisted in 15 themselves in accordance with the invention were taken, using water as the liquid. In the illustration the recorded pump output is represented on the vertical Y-axis and the quantitative flow of the water through the respective tubes is shown on the horizontal X-axis. The curve 8 shows the recorded pump output for different volume flows for conventional cylindrical tubes 20 and the curve 10 shows in comparison the pump output for different volume flows for oval tubes according to the invention. The cross-sectional areas of the cylindrical and oval tubes respectively have remained constant. It can be seen that the recorded pump output in accordance with curve 10 for tubes according to the invention, with the same volume flow, is less 25 than in the case of conventional tubes. Figures 4 and 5 show diagrammatic views of further flow channels according to the invention and flows which are produced therein. With a twist in respect of a flow channel in relation to the diagrammatically indicated longitudinal axis 3 of a flow channel, when a liquid flows 30 therethrough, firstly substantially two larger flow regions 12, 14 are produced, which in the course of the flow are wrapped around in the manner of a double helix. The degree of intermingling of the regions 12, 14 is slight. Within each flow region 12, 14, sub-flow regions 16, 18 and 20, 7 22 respectively are formed, which in turn are again wrapped around in the manner of a double helix. Once again in those sub-flow regions 16 - 20, mutually twisted sub-flow regions can in turn be formed there. As the Figures show the two main flow regions or core flow channels 5 12, 14 are of a substantially round cross-sectional configuration. Adjacent to the core flow channels 12, 14, secondary flows or secondary flow regions 24, 26 can be produced, in which possibly certain components, for example solid constituents, can collect. Separation of constituent parts of the liquid is possible in that way.

Claims (13)

1. A flow channel for liquids characterised in that at least one wall defining the flow channel is of such a configuration that when a liquid flows therethrough at least one flow region is produced which has an axial and simultaneous tangential flow component.
2. A flow channel according to claim 1 characterised in that the wall is of such a configuration that a circulating spiral flow is produced in region wise manner or completely.
3. A flow channel according to claim 1 or claim 2 characterised in that the flow cross-section of the flow channel is non-cylindrical and is twisted in itself in the axial direction so that when the liquid flows therethrough a spiral-form flow is produced at least in region-wise manner.
4. A flow channel according to claim 3 characterised in that the length of a tube portion which is completely wound once in itself (wavelength) is in a given ratio to the length of the smallest bisector of the cross-sectional area of the flow channel, which is in the region of 6 to 7, particularly preferably in the region of 6.44.
5. A flow channel for liquids, in particular according to one of the preceding claims, characterised in that the wall delimiting the flow channel is so shaped that the free flow cross-section of the flow tube is substantially oval.
6. A flow channel according to claim 5 characterised in that the ratio of the length of the longer axis of the oval flow cross-section to the shorter axis of the flow cross-section is greater than 1, preferably greater than or equal to 12. 9
7. A flow channel according to one of the preceding claims characterised in that the flow cross-section decreases in the flow direction.
8. A flow channel according to one of the preceding claims characterised in that the flow cross-section enlarges in the flow direction.
9. A flow channel according to at least one of the preceding claims characterised in that the flow cross-section is quadrangular, triangular, hexagonal or octagonal.
10. A flow channel according to one of the preceding claims characterised in that it is in the form of a tube.
11. A flow channel for liquids, in particular according to one of the preceding claims, wherein the flow channel is so designed that within the channel when a liquid flows therethrough substantially two flow regions are produced, which do not or which scarcely interpenetrate and which are wrapped around in the nature of a double helix.
12. A flow channel according to claim 11 characterised in that within each flow region there are produced further sub-flow regions which in turn are again intertwined with each other.
13. A flow channel according to claim 11 or claim 12 characterised in that the two core flow channels are of a substantially round cross-sectional configuration and form a main fluid flow and that produced in the region of the flow tube which is not occupied by the main flow cores are one or more secondary flows, wherein no or preferably only a slight fluid exchange takes place between a main flow and a secondary flow area and foreign bodies in the entire fluid flow are preferably transported in the secondary flow area.
AU2004267143A 2003-07-22 2004-03-20 Flow channel for liquids Abandoned AU2004267143A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10333477.7 2003-07-22
DE10333477A DE10333477A1 (en) 2003-07-22 2003-07-22 Flow passage for fluids has at least one wall bounding flow passage in such way that with through-flow of fluid at least one flow region is formed which has axial and simultaneously tangential flow component
PCT/EP2004/002961 WO2005019658A1 (en) 2003-07-22 2004-03-20 Flow channel for liquids

Publications (1)

Publication Number Publication Date
AU2004267143A1 true AU2004267143A1 (en) 2005-03-03

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Application Number Title Priority Date Filing Date
AU2004267143A Abandoned AU2004267143A1 (en) 2003-07-22 2004-03-20 Flow channel for liquids

Country Status (17)

Country Link
US (1) US7487799B2 (en)
EP (1) EP1649173A1 (en)
JP (1) JP2006528750A (en)
KR (1) KR20060036468A (en)
CN (1) CN1833109A (en)
AR (1) AR046398A1 (en)
AU (1) AU2004267143A1 (en)
BR (1) BRPI0412883A (en)
CA (1) CA2533042A1 (en)
DE (1) DE10333477A1 (en)
EG (1) EG23928A (en)
IL (1) IL173185A0 (en)
IS (1) IS8317A (en)
MX (1) MXPA06000733A (en)
NO (1) NO20060842L (en)
WO (1) WO2005019658A1 (en)
ZA (1) ZA200600103B (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080237044A1 (en) * 2007-03-28 2008-10-02 The Charles Stark Draper Laboratory, Inc. Method and apparatus for concentrating molecules
WO2008130618A1 (en) 2007-04-19 2008-10-30 The Charles Stark Draper Laboratory, Inc. Method and apparatus for separating particles, cells, molecules and particulates
US7837379B2 (en) * 2007-08-13 2010-11-23 The Charles Stark Draper Laboratory, Inc. Devices for producing a continuously flowing concentration gradient in laminar flow
CA2750285C (en) * 2009-01-21 2016-12-13 Sumitomo Metal Industries, Ltd. Hollow member
US20100278666A1 (en) * 2009-04-30 2010-11-04 Olson David A High solids material moving apparatus
DE102009058198A1 (en) 2009-12-15 2011-06-16 Sms Siemag Ag Nozzle device and strand guiding device with the nozzle device
DE202011110064U1 (en) 2011-06-07 2012-11-16 Sms Siemag Ag Nozzle device and strand guiding device with the nozzle device
CN103204186B (en) * 2012-01-17 2016-04-20 朱晓义 Running gear
JP2014198324A (en) * 2013-03-29 2014-10-23 ソニー株式会社 Microfluidic channel and microfluidic device
CN104386236A (en) 2014-11-17 2015-03-04 朱晓义 Aircraft with great lift force
DE102015010639B4 (en) * 2015-08-13 2019-01-31 Sandy Schöbbel Use of a tube
EP3587987B1 (en) * 2017-06-07 2023-02-15 Nanjing Tech University Pipe-type mixer
US11187466B2 (en) * 2019-07-26 2021-11-30 Denso International America, Inc. Heat exchanger and heat exchanging system
CN111151390A (en) * 2020-01-22 2020-05-15 柯敏兴 Liquid goes out liquid shape controlling means
RU2739626C1 (en) * 2020-03-23 2020-12-28 Борис Никифорович Сушенцев Method for reduction of hull hydrodynamic resistance and high-speed vessel using method thereof
CN112870960A (en) * 2021-03-19 2021-06-01 中国华电科工集团有限公司 Ammonia spraying device and flue gas denitration device
CN113390209B (en) * 2021-07-07 2022-06-24 内蒙古大唐国际克什克腾煤制天然气有限责任公司 Device and method for supplementing refrigerant to refrigerating system without pressurizing equipment in winter

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US770599A (en) * 1904-09-20 Half to e
US85149A (en) * 1868-12-22 Improvement in tubes for steam-generators
US862919A (en) * 1905-06-23 1907-08-13 Rifled Pipe Company Helically-corrugated pipe.
US1363416A (en) * 1918-09-24 1920-12-28 Ross B Hooker Method of making radiator-tubes
US1958577A (en) * 1930-06-12 1934-05-15 Glarence F Hirshfeld Apparatus for dust separation
AT134543B (en) 1931-08-12 1933-08-25 Viktor Schauberger Water flow in pipes and channels.
GB409528A (en) 1933-06-28 1934-05-03 Aerol Engine Corp Improvements in liquid conducting conduits
US2139888A (en) * 1936-08-10 1938-12-13 Arthur J Fausek Hose structure
US2115769A (en) * 1936-08-22 1938-05-03 Henry H Harris Radiant heating tube
US2115796A (en) * 1937-01-06 1938-05-03 American Car & Foundry Co Locking mechanism for venetian blinds
FR1002454A (en) 1946-10-04 1952-03-06 Schnellbau Technik G M B H Circulation pipe, in particular for gas and / or powder mixtures
US2935906A (en) * 1957-07-01 1960-05-10 Andreasson Rudolf William Oil tube drill
US3273916A (en) * 1961-03-13 1966-09-20 Lloyd E Tillery Unitary flexible metallic connector
US3224814A (en) * 1962-12-03 1965-12-21 Sprout Waldron & Co Inc Conduit for pneumatic conveying systems
US3612175A (en) * 1969-07-01 1971-10-12 Olin Corp Corrugated metal tubing
US3578075A (en) * 1969-10-29 1971-05-11 Olin Corp Corrugated tubing
US3743328A (en) * 1971-07-26 1973-07-03 E Longfellow Gas appliance connector
DE2156578B2 (en) * 1971-11-15 1980-12-11 Knut Dr.-Ing. 3000 Hannover Kauder Flexible heat exchanger piping
DE2510169A1 (en) 1975-03-08 1976-09-16 Albert Ziegler Kg Fluid hose or pipe - has projecting strip part on inner wall of line coiling around itself
US4979296A (en) * 1986-07-25 1990-12-25 Shell Oil Company Method for fabricating helical flowline bundles
US4843713A (en) * 1986-07-25 1989-07-04 Shell Oil Company Apparatus for making helical flowline bundles
CA1328040C (en) * 1986-07-25 1994-03-29 Carl Gottlieb Langner Fabricating helical flowline bundles
WO1990015256A1 (en) 1989-06-07 1990-12-13 Aerosep Societe Anonyme Curved fluid translation systems
FR2708327B1 (en) * 1993-07-01 1995-10-13 Hutchinson Tubular profile, for use as a seal, muffler or flexible conduit for motor vehicles.
DE19806513A1 (en) * 1998-02-17 1999-08-19 Evert Design elements to improve flow of fluid in tubes
GB9828696D0 (en) * 1998-12-29 1999-02-17 Houston J G Blood-flow tubing
WO2001018406A1 (en) * 1999-09-09 2001-03-15 Brown Fintube Improved tube for heat exchangers
US7264394B1 (en) * 2002-06-10 2007-09-04 Inflowsion L.L.C. Static device and method of making
US20040134557A1 (en) * 2002-06-28 2004-07-15 Cymbalisty Lubomyr M. Hydrodynamic static mixing apparatus and method for use thereof in transporting, conditioning and separating oil sands and the like
CA2411220C (en) * 2002-06-28 2010-11-16 Lubomyr M. Cymbalisty Hydro-dynamic static mixing apparatus and method for use thereof in separating oil sands and the like
US6997214B2 (en) * 2004-07-07 2006-02-14 Lin Lin Kuo Intake tubing for engines

Also Published As

Publication number Publication date
JP2006528750A (en) 2006-12-21
US7487799B2 (en) 2009-02-10
ZA200600103B (en) 2006-09-27
MXPA06000733A (en) 2006-04-19
US20070017588A1 (en) 2007-01-25
IL173185A0 (en) 2006-06-11
IS8317A (en) 2006-02-21
WO2005019658A1 (en) 2005-03-03
EP1649173A1 (en) 2006-04-26
DE10333477A1 (en) 2005-02-24
CN1833109A (en) 2006-09-13
BRPI0412883A (en) 2006-10-03
EG23928A (en) 2008-01-13
CA2533042A1 (en) 2005-03-03
KR20060036468A (en) 2006-04-28
NO20060842L (en) 2006-03-15
AR046398A1 (en) 2005-12-07

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MK4 Application lapsed section 142(2)(d) - no continuation fee paid for the application